▸Orbital parameters

Orbit class	SSO
Inclination	97.9955°
Eccentricity	0.0003410
Period	98.1 min
Apogee	669 km
Perigee	664 km
Mean motion	14.68303732 rev/day
RAAN	242.1750°
Arg of perigee	42.1958°
Mean anomaly	317.9509°
B*	6.8922e-5
Rev at epoch	12,773

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 58987U 24032A 26187.93138774 .00000350 00000-0 68922-4 0 9993

2 58987 97.9955 242.1750 0003410 42.1958 317.9509 14.68303732127732

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CE-SAT-IE",
  "OBJECT_ID": "2024-032A",
  "EPOCH": "2026-07-06T22:21:11.901+00:00",
  "MEAN_MOTION": 14.68303732,
  "ECCENTRICITY": 0.000341,
  "INCLINATION": 97.9955,
  "RA_OF_ASC_NODE": 242.175,
  "ARG_OF_PERICENTER": 42.1958,
  "MEAN_ANOMALY": 317.9509,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58987,
  "REV_AT_EPOCH": 12773,
  "BSTAR": 0.000068922,
  "MEAN_MOTION_DOT": 0.0000035,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	CE-SAT-IE
Operator	Canon Electronics Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Japan
Launch date	Feb 17, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	70HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/58987

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.